Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

A flying car wing retractable system

A flying car and wing technology, applied in the field of flying car wing retractable system, can solve the problems of high cost, complex and cumbersome system, and large overall weight

Inactive Publication Date: 2020-05-01
BEIHANG UNIV
View PDF5 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, the most commonly used folding unfolding and folding scheme adopts the wing unfolding and folding scheme of a military carrier-based aircraft, which uses a hydraulic system and a connecting rod system, but it has the following problems: the overall weight is large and the system is complicated It is cumbersome and costly, so it is suitable for military use, and it is difficult and easy to apply to civilian flying cars

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • A flying car wing retractable system
  • A flying car wing retractable system
  • A flying car wing retractable system

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0032] The purpose of the present invention is to provide a wing retractable system for a flying car. The provided wing retractable system is safe and reliable, has a simple structure, low manufacturing cost, and is convenient for civil and commercial use.

[0033] In order to enable those skilled in the art to better understand the technical solutions of the present invention, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0034] Such as Figure 1-4 as shown, figure 1 It is a structural schematic diagram of a specific embodiment of the flying car wing retractable system provided by the present invention, figure 2 for figure 1 A schematic diagram of the structure of a retractable locking mechanism, image 3 for figure 2 A cross-sectional view of the A-A direction, Figure 4 for figure 1 Schematic diagram of the structure of the anti-interference mechanism.

[0035] In this specifi...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention discloses a flying automobile wing contraction-release system, comprising a contraction-release guide mechanism, two contraction-release locking mechanisms and two skin anti-interferencemechanisms; the contraction-release guide mechanism is used for contracting, releasing and rotating wings; the two contraction-release locking mechanisms are used for ensuring safety and reliabilityfor the contraction and release of the wings; the two skin anti-interference mechanisms are used for ensuring completeness of pneumatic contours of the wings. The flying automobile wing contraction-release system is good in safety and reliability, simple in structure, low in manufacture cost and easy to use for civil and commercial purposes.

Description

technical field [0001] The invention relates to the field of flying cars, and can also be applied to aircrafts such as airplanes with wings, and in particular relates to a flying car wing retractable system. Background technique [0002] Flying cars take up a lot of space when driving and parking on the ground, which is inconvenient. In addition, for flying cars with wings, they need to be folded and stowed when driving on the ground to meet the requirements of national road regulations. The wings are then extended to meet the aerodynamic demands of flight. Therefore, setting up a safe and reliable system capable of unfolding and folding wings for the above-mentioned aircraft has become a technical problem urgently to be solved in this technical field. [0003] At present, the most commonly used folding unfolding and folding scheme adopts the wing unfolding and folding scheme of a military carrier-based aircraft, which uses a hydraulic system and a connecting rod system, bu...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Patents(China)
IPC IPC(8): B60F5/02B64C3/56
CPCB60F5/02B64C3/56
Inventor 林海英吴帅李泽宇
Owner BEIHANG UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com